View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67551U 26145.38319466 +.00000000 +00000-0 +96094-3 0 00006
2 67551 97.2863 32.3762 0001834 92.6145 267.5307 15.33459184 00
| Epoch (UTC): | 25 May 2026 09:11:48 |
| Eccentricity: | 0.0001834 |
| inclination: | 97.2863° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.3762° |
| argument of perigee: | 92.6145° |
| revolutions per day: | 15.33459184 |
| mean anomaly at epoch: | 267.5307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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